发明名称 |
SINGLE-SHAFT GAS-TURBINE PLANT |
摘要 |
gas-turbine plants. SUBSTANCE: single- shaft gas-turbine plant with multi-stage rotor includes disks with working blades and intermediate disks. Blade safety locks with cylindrical axial projections received by mating holes in rim of adjacent intermediate disk are fitted in slots of disk rim of last stage of rotor. EFFECT: enhanced reliability due to locking intermediate disks relative to disks with working blades in circumferential direction; enhanced maintainability due to knockdown construction of rotor. 4 dwg
|
申请公布号 |
RU2166640(C2) |
申请公布日期 |
2001.05.10 |
申请号 |
RU19990111336 |
申请日期 |
1999.05.25 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "AVIADVIGATEL'" |
发明人 |
INOZEMTSEV A.A.;SULIMOV D.D.;KUZNETSOV V.A.;TOROPCHIN S.V. |
分类号 |
F01D5/30 |
主分类号 |
F01D5/30 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|